Intermittent type swirl injection nozzle

Claim 1

An intermittent type swirl injection nozzle comprising: a nozzle body comprising a guide hole and a bottom portion on which a spray hole and a body seat are formed; a fuel supply source for supplying fuel; a needle valve slidably inserted and reciprocally moved within said guide hole of said nozzle body, said needle valve having a tip portion for seating on said body seat to open and close said spray hole; a swirl chamber formed downstream of said fuel supply source and upstream of said spray hole, said swirl chamber being defined between said nozzle body and said needle valve, and said swirl chamber communicating with said spray hole when said tip portion of said needle valve is not seated on said body seat, and said tip portion of said needle valve being located downstream of said swirl chamber when said tip portion is seated on said body seat; a swirl passage connected to said swirl chamber and provided around a longitudinal axis of said needle valve for giving a swirl flow influence around said axis of said needle valve to fuel flowing when said needle valve is lifted from said body seat to open said spray hole; a straight passage connected to said swirl chamber and provided between said nozzle body and said needle valve in a region where they slidably contact for giving the fuel a straight flow influence in an axial direction of said needle valve; inlet means, provided downstream of said fuel supply source and upstream of said swirl chamber, for communicating said fuel supply source with said straight passage and said swirl passage; and means (4) for separating said straight passage from said swirl passage and preventing the fuel having the swirl flow influence from mixing with the fuel having the straight flow influence before entering said swirl chamber, said separating means being disposed between said nozzle body and said needle valve, wherein said swirl and straight passages satisfy at least one of the following conditions: (1) the sum of first and second effective flow areas (K 1 +K 2 ) of said swirl and straight passages relative to a third effective flow area (K 3 ) of said spray hole is within a range of 1 to 5; (2) the first effective flow area (K 1 ) of said swirl passage relative to the second effective flow area (K 2 ) of said straight passage is within a range of 0.2 to 2; (3) the angle (φ 1 ) of said swirl passage relative to the axis of said needle valve is within a range of 5° to 60°; and (4) the fuel pressure (P 2 ) in said swirl chamber relative to the fuel pressure (P 1 ) at said inlet means is within a range of 0.4 to 0.95, and wherein said swirl passage is defined between said separating means and an inner surface of said nozzle body which faces said needle valve, and said straight passage is defined between said needle valve and said separating means.